(2) Do this test:
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the center pedestal on the On the aircraft:
panel 114VU:
- move the slat and flap control - the flaps and slats move to their set
lever to position 1 and then to positions.
position 2. Stop at both
notches until the flaps and On the ECAM upper DU:
slats are in their new - the flap and slat position bars move
position. to their set positions
- the new position of the control lever
and the travel direction of the flaps
and slats are shown.
2. On the panel 114VU: On the aircraft:
- move the slat and flap control - the flaps move to the set position
lever to the position 3. - the slats do not move.
On the ECAM upper DU:
- the flap position bar moves to the
set position
- the slat position bar does not move
- the new position of the control lever
and the travel direction of the flaps
are shown.
3. On the panel 114VU: On the aircraft:
- move the slat and flap control - the flaps and slats move to their set
lever to the position FULL. positions.
On the ECAM upper DU:
- the flap and slat position bars move
to their set positions
- the new position of the control lever
and the travel direction of the flaps
and slats are shown.
4. On the panel 114VU: On the aircraft:
1EFF : ALL 1 27-54-00Page 509 1 1 May 01/04R 1 1 1CES 1
-------------------------------------------------------------------------------
ACTION RESULT -------------------------------------------------------------------------------
-move the slat and flap control
lever back to the position 3.
5. On the panel 114VU:
-move the slat and flap control lever back to the position 2.
6. On the panel 114VU:
-move the slat and flap control lever back to the positions 1 and 0. Stop at both notches until the flaps and slats are in their new position.
-
the flaps and slats move to their setpositions.
On the ECAM upper DU:
-
the flap and slat position bars move to their set positions
-
the new position of the control lever and the travel direction of the flaps and slats are shown.
On the aircraft:
-
the flaps move to the set position
-
the slats do not move.
On the ECAM upper DU:
-
the flap position bar moves to the set position
-
the slat position bar does not move
-
the new position of the control lever and the travel direction of the flaps are shown.
On the aircraft:
-
the flaps and slats move to their setpositions.
On the ECAM upper DU:
-
the flap and slat position bars move to their set positions
-
the new position of the control lever and the travel direction of the flaps and slats are shown
-no warnings related to the flap and slat systems are shown.
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5. Close-up________
Subtask 27-54-00-860-068
A. Aircraft Maintenance Configuration
(1) Depressurize the Yellow hydraulic system (Ref. TASK 29-10-00-864-002).
(2) Depressurize the Blue hydraulic system (Ref. TASK 29-10-00-864-003).
(3) If applicable, connect the PTU (Ref. TASK 29-23-00-860-002).
(4) Do the EIS stop procedure (Ref. TASK 31-60-00-860-002).
(5) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
R Subtask 27-54-00-865-079
R R R B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 14CC1, 14CC2
Subtask 27-54-00-942-069
R C. Removal of Equipment
(1) Make sure that the work area is clean and clear of tool(s) and other items.
(2) Remove the safety barriers.
(3) Remove the warning notice(s).
(4) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
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本文鏈接地址：A320飛機(jī)維護(hù)手冊(cè) AMM FLIGHT CONTROLS 飛行操縱4(149)
